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Fatigue crack growth aluminum alloys

Y. Xue et al Micromechanisms of multistage fatigue crack growth in a high-strength aluminum alloy. Acta Mater. 55, 1975-1984 (2007)... [Pg.134]

Fie. 7.125 Corrosion-fatigue-crack-growth rate as a function of stress-in-tensity range for a high-strength aluminum alloy in dry argon and indicated halide solutions. Source Ref 1 73... [Pg.437]

Moisture-Enhanced Fatigue Crack Growth in Aluminum Alloys [1,2, 5]... [Pg.165]

Figure 9.2. Influence of water vapor pressure (or pressure/frequency) on fatigue crack growth rates in 2219-T851 aluminum alloy at room temperature. Solid line represents model predictions [2]. Figure 9.2. Influence of water vapor pressure (or pressure/frequency) on fatigue crack growth rates in 2219-T851 aluminum alloy at room temperature. Solid line represents model predictions [2].
Figure 9.6. The influence of water vapor pressure on fatigue crack growth rate in I/M 7075-T651 aluminum alloy at room temperature [5]. Figure 9.6. The influence of water vapor pressure on fatigue crack growth rate in I/M 7075-T651 aluminum alloy at room temperature [5].
Bradshaw, F. J., and Wheeler, C., The Effect of Environment on Fatigue Crack Growth in Aluminum and Some Aluminum Alloys, Applied Materials Research, 5 (1966), 112-120. [Pg.181]

Gao, M., Pao, P. S., and Wei, R. P., Chemical and Metallurgical Aspects of Environmentally Assisted Fatigue Crack Growth in 7075-T651 Aluminum Alloy, Met. Trans. A, 19A... [Pg.208]

Papakyriacou, M., Mayer, H., Fuchs, U., Stanzl-Tschegg, S. E., and Wei, R. P., Influence of Atmospheric Moisture on Slow Fatigue Crack Growth at Ultrasonic Frequency in Aluminum and Magnesium Alloys, Blackwell Science Ltd. Fatigue Fract Engng Mater Struct 25 (2002), 795-804. [Pg.211]

The fatigue crack growth rate test results on AMg6 aluminum alloy at 4 K, 76 K, and room temperature, are summarized in Figs. 3,4, and 5, respectively. The Paris power law [ ] is used as the basis for empirical analysis of the data... [Pg.521]

The fatigue crack growth rates and the fracture toughness of AMg6 aluminum alloy have been determined at room temperature, 76 K, and 4K. The results indicate that ... [Pg.527]

DuQuesnay, D. L., UnderhiU, P. R., and Britt, H. J., Fatigue Crack Growth from Corrosion Damage in 7075-T65511 Aluminum Alloy Under Aircraft Loading, International Journal of Fatigue, Vol. 25, 2003, pp. 371-377. [Pg.318]

Ambriz, R.R., Mesmacque, G., Benhamena, A., Ruiz, A., Amrouche, A., Lopez, V.H. Fatigue Crack Growth Behaviour in 6061-T6 Aluminum alloy welds obtained by MIEA... [Pg.582]

The SCC behavior of a high-strength aluminum alloy in several environments is shown in Fig. 7.113. The effect of cyclic stress-intensity range, AK, on the growth of fatigue cracks in the same high-strength aluminum alloy and in similar environments is shown in Fig. 7.125 (Ref 173). The similarity in the shapes of the two sets of curves should be... [Pg.436]

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See also in sourсe #XX -- [ Pg.550 ]



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